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US-2000-06-01 : Fuel Strainer Assembly Inspection

Number US-2000-06-01
Issued by United States of America  United States of America
Issue date 2000-03-22
Effective date 2000-05-05
EASA approval number
ATA Chapter 28
Approval Holder
/ Type Designation
  • TEXTRON AVIATION INC.
    • 150
      • 150F
      • 150G
      • 150H
      • 150J
      • 150K
      • 150L
      • 150M
      • A150K
      • A150L
      • A150M
    • 152
      • 152
      • A152
    • 172 (Skyhawk)
      • 172F
      • 172G
      • 172H
      • 172I
      • 172K
      • 172L
      • 172M
      • 172N
      • 172P
      • 172Q
    • 172RG
    • 177 (Cardinal)
      • 177
      • 177A
      • 177B
    • 177RG (Cardinal RG)
    • 180
      • 180H
      • 180J
      • 180K
    • 182 (Skylane)
      • 182H
      • 182J
      • 182K
      • 182L
      • 182M
      • 182N
      • 182P
      • 182Q
      • 182R
      • R182
      • T182
      • TR182
    • 185 (Skywagon)
      • 185D
      • 185E
      • A185E
      • A185F
    • 188 (AGwagon)
      • 188
      • 188A
      • 188B
      • A188
      • A188A
      • A188B
      • T188C
    • 206/U206 (Super Skywagon)
      • TU206A
      • TU206B
      • TU206C
      • TU206D
      • TU206E
      • TU206F
      • TU206G
      • U206
      • U206A
      • U206B
      • U206C
      • U206D
      • U206E
      • U206F
      • U206G
    • 207 (Skywagon)
      • 207
      • 207A
      • T207
      • T207A
    • 210 (Centurion)
      • 210E
      • 210F
      • 210G
      • 210H
      • 210J
      • 210K
      • 210L
      • 210M
      • 210N
      • P210N
      • T210F
      • T210G
      • T210H
      • T210J
      • T210K
      • T210L
      • T210M
      • T210N
    • 337 (Super Skymaster)
      • 337
      • 337A
      • 337B
      • 337C
      • 337D
      • 337E
      • 337F
      • 337G
      • 337H
      • M337B
      • P337H
    • P206/TP206 (Super Skylane)
      • P206
      • P206A
      • P206B
      • P206C
      • P206D
      • P206E
      • TP206A
      • TP206B
      • TP206C
      • TP206D
      • TP206E
    • R172 (Hawk XP)
      • R172E
      • R172F
      • R172G
      • R172H
      • R172J
      • R172K
    • T337
      • T337B
      • T337C
      • T337D
      • T337E
      • T337F
      • T337G
      • T337H
      • T337H-SP
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Cessna Single Engine SB No. SEB97-9, dated November 17, 1997, or Multi-engine SB No. MEB97-12, dated November 17, 1997. Copies may be obtained from the Cessna Aircraft Company, P. O. Box 7706, Wichita, Kansas 67277.
Remarks This AD is not the State of Design AD for France-manufactured (Reims Aviation) aeroplanes - see DGAC France AD 2000-529 (F-2000-529) and AD 2000-525 (F-2000-525), both issued 27 December 2000. This AD does not apply to Argentina-manufactured aeroplanes, which are not validated in Europe. Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu.

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